KR101703962B1 - Sliding element, in particular piston ring, and combination of a sliding element with mating running element - Google Patents

Sliding element, in particular piston ring, and combination of a sliding element with mating running element Download PDF

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KR101703962B1
KR101703962B1 KR1020127012367A KR20127012367A KR101703962B1 KR 101703962 B1 KR101703962 B1 KR 101703962B1 KR 1020127012367 A KR1020127012367 A KR 1020127012367A KR 20127012367 A KR20127012367 A KR 20127012367A KR 101703962 B1 KR101703962 B1 KR 101703962B1
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layer
metal
dlc
sliding element
piston ring
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KR20120091212A (en
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마르쿠스 케네디
마이클 지느나보르드
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페데랄-모굴 부르샤이트 게엠베하
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J9/00Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
    • F16J9/26Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/22Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
    • C23C16/26Deposition of carbon only
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/02Pretreatment of the material to be coated
    • C23C16/0272Deposition of sub-layers, e.g. to promote the adhesion of the main coating
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C16/00Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
    • C23C16/02Pretreatment of the material to be coated
    • C23C16/0272Deposition of sub-layers, e.g. to promote the adhesion of the main coating
    • C23C16/029Graded interfaces
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/04Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
    • C23C28/044Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material coatings specially adapted for cutting tools or wear applications
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/04Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material
    • C23C28/046Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings of inorganic non-metallic material with at least one amorphous inorganic material layer, e.g. DLC, a-C:H, a-C:Me, the layer being doped or not
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F5/00Piston rings, e.g. associated with piston crown

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Physical Vapour Deposition (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

본 발명은 슬라이딩 요소에 관한 것으로서, 주철, 또는 내측으로부터 외측으로 연장하는 CrN 층, Me(CxNy) 층 및 DLC 층를 가진 코팅을 구비하는 금속으로 제조된 피스톤 링에 있어서, DLC 층는 금속을 사용하지 않는(metal-free) DLC 층 또는 금속-함유 하부구조 및 금속을 사용하지 않는 DLC 상부층으로 구성된다. 본 발명은 이러한 슬라이딩 요소와 상대 작동 요소의 조합에 관한 것이다.The present invention relates to a sliding element, comprising: a piston ring made of a metal having a coating with a cast iron or a CrN layer extending outwardly from the inside, a layer Me (C x N y ) and a DLC layer, A metal-free DLC layer or a metal-containing substructure and a metal-free DLC upper layer. The present invention relates to a combination of such a sliding element and a relative operating element.

Description

슬라이딩 요소 특히, 피스톤 링, 및 슬라이딩 요소와 상대 작동 요소의 조합{Sliding element, in particular piston ring, and combination of a sliding element with mating running element}A sliding element, in particular a piston ring, and a combination of a sliding element and a relative operating element,

본 발명은 슬라이딩 요소 특히, 코팅을 구비하는 피스톤 링, 및 슬라이딩 요소와 상대 작동 요소(mating running element)의 조합에 관한 것이다. The invention relates to a sliding element, in particular a piston ring with a coating, and a combination of a sliding element and a mating running element.

상대 작동 요소와 접촉하는 슬라이딩 요소는 여러 가지 기술 분야에 적용된다. 피스톤 링과 실린더 라이너의 조합은 전형적인 예로 간주 될 수 있다. 만약, 실린더들 또는 실린더 라이너들이 예를 들어, 알루미늄-실리콘 합급으로 제조되는 경우, 특히 불꽃-점화 기관, DLC(diamond like carbon) 코팅 시스템에서 마모 및 마찰 손실에 대하여 그 가치가 입증되었다. 그러나, 알려진 DLC 층 시스템들은 철계(iron-based) 실린더 라이너들을 가진 디젤 엔진 또는 고출력 과급기를 가진 불꽃-점화 기관에 사용하기 위한 사용 연한 및 적합성과 관련하여 개선의 필요성이 있다. 엄청나게 높은 실린더 압력과 특히, 직접 분사의 결합 때문에, 혼합된 마찰 상태의 더 큰 비례가 존재한다. 이러한 유형의 상황을 위한 DLC 코팅 시스템의 부적절한 안정성을 위한 결정적인 요인은 층 두께가 대체적으로 5㎛ 미만으로 고려되어야 한다. The sliding element in contact with the counterpart actuating element is applied in various technical fields. The combination of a piston ring and a cylinder liner can be considered as a typical example. If the cylinders or cylinder liners are made of, for example, aluminum-silicon alloys, their value has been demonstrated for wear and friction losses, especially in spark-ignition engines, diamond like carbon (DLC) coating systems. However, the known DLC layer systems have a need for improvement in terms of service life and suitability for use in diesel engines with iron-based cylinder liners or flame-ignition engines with high power superchargers. Due to the extremely high cylinder pressure and especially the combination of direct injection, there is a greater proportion of the mixed friction state. A crucial factor for the improper stability of the DLC coating system for this type of situation is that the layer thickness should generally be considered to be less than 5 [mu] m.

DE 10 2005 063 123 B3은 런-인(run-in) 층로 코팅된 DLC를 개시한다. 더 큰 층 두께와 관련하여, 특히, 10-30㎛의 층 두께를 가진 CrN 계열의, PVD 코팅들이 알려져 있다. 비록 이러한 것들은 수명 연한을 개선할 수 있지만, 마찰 손실 내마모성이 악화되고, 특히 불충분한 윤활 작용과 내흠집성의 악화된다. 반면에, 그들의 비결정질 구조 때문에, DLC 층 시스템은 금속 표면에 대해 화학적으로 실질적으로 비활성이기 때문에 상대 작동 요소에 대해 극도로 낮은 접착성의 경향을 나타내는 장점을 가진다. DE 10 2005 063 123 B3 discloses a DLC coated with a run-in layer. With respect to larger layer thicknesses, in particular, PVD coatings of the CrN series with a layer thickness of 10-30 mu m are known. Although these can improve the service life, the friction loss abrasion resistance deteriorates, and in particular, the insufficient lubrication performance and the scratch resistance deteriorate. On the other hand, due to their amorphous structure, the DLC layer system has the advantage of exhibiting an extremely low adhesion tendency to the relative operating elements, since it is chemically substantially inert to the metal surface.

DE 296 05 666 U1은 금속을 포함하지 않는(metal-free), 층 두께에 대해 등급이 매겨진 경도를 가진 비결정질 카본 층으로 코팅된 내연 기관의 영역의 성분과 관련된다. DE 296 05 666 U1 relates to the constituents of the region of the internal combustion engine coated with an amorphous carbon layer having a hardness graded against the layer thickness, which is metal-free.

DE 10 2008 016 864 B3은 내측으로부터 외측으로 연장하는 접착 층, 금속-함유 비결정질 카본 층 및 금속을 포함하지 않는 비결정질 카본 층을 구비하는 피스톤 링을 개시한다.DE 10 2008 016 864 B3 discloses a piston ring comprising an adhesive layer extending from the inside to the outside, a metal-containing amorphous carbon layer and an amorphous carbon layer not containing a metal.

WO 2009/106201 A1은 DLC 커플링 에이전트 층, DLC 기능 층 및 DLC 런-인 층들이 기재에 존재하는 내연 기관의 요소에 관련된다.WO 2009/106201 A1 relates to elements of an internal combustion engine in which a DLC coupling agent layer, a DLC functional layer and DLC run-in layers are present in a substrate.

마지막으로, WO 2006/125683 A1은 내측으로부터 외측으로 연장하는 1VB, VB 또는 V1B 그룹들로부터 하나의 요소를 가진 층, 다이아몬드-유사 나노복합 조성물 및 DLC 층를 구비하는 피스톤 링을 개시한다.Finally, WO 2006/125683 A1 discloses a piston ring having a layer with one element from 1VB, VB or V1B groups extending outward from the inside, a diamond-like nanocomposite composition and a DLC layer.

본 발명은 예를 들어, 철계 상대 작동 요소와 함께 특히, 디젤 엔진 또는 고출력 과급기를 가진 불꽃-점화 기관에 사용될 때, 사용 연한과 마찰 손실과 관련된 요구조건들을 달성하는 슬라이딩 요소 특히, 피스톤 링을 제공하는 것을 그 기술적 과제로 한다. The present invention provides a sliding element, particularly a piston ring, which, when used, for example, in a spark-ignition engine with a diesel engine or a high-power supercharger, together with an iron-based relative operating element, achieves requirements relating to wear and friction losses As a technical problem.

또한, 본 발명은 슬라이딩 요소와 상대 작동 요소의 적절한 조합을 개시한다.The present invention also discloses an appropriate combination of sliding elements and relative working elements.

본 발명의 상술한 목적은 청구항 1에 개시된 슬라이딩 요소에 의해 달성된다.The above-mentioned object of the present invention is achieved by the sliding element disclosed in claim 1.

한편으로는, 이러한 슬라이딩 요소는 CrN 층과 외측에 있는 DLC 층의 조합을 특징으로 한다. DLC 층은 금속을 포함하지 않거나 금속-함유 하부구조(substructure) 및 금속을 포함하지 않는 DLC 상부층을 구비하는 어느 하나이다. 다시 말해, DLC 층은 적어도 부분적으로 금속을 포함하지 않고, 특히, 외면에서, 금속을 포함하지 않는 DLC 층을 구비한다. 또한, 대규모의 실험들에 의하면, 개시된 코팅은 Me(CxNy)층이 CrN층과 DLC층 사이의 중간층으로서 제공될 때, 특히 양호한 특성을 나태는 것을 보여준다. 이러한 층 구조를 사용한 시험들은 슬라이딩 요소 특히, 피스톤 링의 표면의 마모 특성이 Cr 접착 층과 DLC 상부층을 구비하는 알려진 구조와 비교하여 향상되었음을 나타낸다. 이것은 내구 연한을 현저하게 향상시킬 수 있다. 또한, 시험들은 상대적 기능 계수를 현저하게 감소시킬 수 있음을 보여준다. On the one hand, this sliding element is characterized by a combination of a CrN layer and an outer DLC layer. The DLC layer is either a metal-free or metal-containing substructure and a DLC top layer that does not contain a metal. In other words, the DLC layer at least partially contains no metal, and in particular, on the outer surface, a DLC layer that does not contain a metal. Also, according to large scale experiments, the disclosed coatings show particularly good properties when the Me (C x N y ) layer is provided as an interlayer between the CrN layer and the DLC layer. Tests using this layered structure indicate that the wear characteristics of the sliding elements, particularly the surfaces of the piston rings, are improved compared to known structures comprising a Cr adhesive layer and a DLC top layer. This can significantly improve durability. The tests also show that the relative functional coefficients can be significantly reduced.

따라서, 대체로, 개시된 층 구조는 향상된 슬라이딩 요소를 제공할 수 있다. CrN 층은 접착층 없이 예를 들어, 금속 증착법 또는 스퍼터링에 의해 기본적인 피스톤 재질에 부가되는 것이 바람직하다. 그러나, 특수한 적용에서, CrN 층은 접착층에 의해 슬라이딩 요소의 기본 재질에 부가될 수 있다.Thus, in general, the disclosed layer structure can provide improved sliding elements. The CrN layer is preferably added to the basic piston material without an adhesive layer, for example by metal deposition or sputtering. However, in special applications, the CrN layer can be added to the base material of the sliding element by the adhesive layer.

명확성을 기하기 위해, Me는 금속을 나타내고, 이것은 예를 들어, 텅스텐, 크로뮴, 티타늄 또는 실리콘일 수 있음을 유의해야 한다. 또한, 카본 및 질소는 사실상 그 어떤 비율로도 전술한 층에 존재할 수 있으며, x와 y는 0-99 원자%(atom %)의 범위일 수 있다. 또한, 특히 적어도 일부 영역에서, 코팅은 천이 표면으로 연장하여 적어도 하나의 러닝 표면(running surface)에 인접한 표면으로 연장할 수 있다. 이것은 예를 들어, 피스톤 링의 러닝 에지(running edges)와 관련된다.For the sake of clarity, it should be noted that Me represents a metal, which may be, for example, tungsten, chromium, titanium or silicon. In addition, carbon and nitrogen can be present in virtually any proportion in the aforementioned layers, and x and y can range from 0 to 99 atomic% (atomic%). Also, particularly in at least some areas, the coating may extend to the transition surface and extend to the surface adjacent to the at least one running surface. This relates, for example, to the running edges of the piston ring.

바람직한 개선 사항들은 다른 청구항들에 개시된다.Preferred improvements are disclosed in other claims.

1100-1900 HV 0.002 값들은 CrN층 또는 하부구조의 경도에 적합한 것으로 판명되었다. 이러한 실시예는 1700-2900 HV 0.002의 금속을 포함하지 않는 DLC층의 경도 및/또는 800-1600 HV 0.002 금속-함유 DLC의 경도와 결합될 수 있다.Values of 1100-1900 HV 0.002 were found to be suitable for the hardness of the CrN layer or substructure. This embodiment can be combined with the hardness of the DLC layer not containing 1700-2900 HV 0.002 metal and / or the hardness of 800-1600 HV 0.002 metal-containing DLC.

또한, DLC-층 특히, 금속-함유 및/또는 금속을 포함하지 않는 DLC 층의 특히 양호한 성질들은 그것이 수소를 함유하는 경우 얻어질 수 있을 것으로 기대된다.In addition, particularly good properties of the DLC-layer, especially the metal-containing and / or metal-free DLC layer, are expected to be obtained if it contains hydrogen.

바람직하게, 금속-함유 DLC층은 예를 들어, WC, CrC, SiC, GeC 또는 TiC와 같은 나노크리스탈 금속카바이드 침전물을 구비할 수 있다. Preferably, the metal-containing DLC layer may comprise nanocrystalline metal carbide precipitates, such as, for example, WC, CrC, SiC, GeC or TiC.

유리한 속성들은 1-30㎛의 두께를 가진 CrN, 2㎛의 최대 두께를 가진 Me(CxNy) 층들 및 5-40㎛의 두께의 전체 층에서 확인되었다.Favorable properties was confirmed in the entire layer of the thickness of the CrN, 2㎛ up Me (C x N y) having a thickness of layers and having a thickness of 1-30㎛ 5-40㎛.

거칠기와 관련하여, 그 성질을 더 개량하기 위해, 거칠기 파라미터들 Rz < 5 및/또는 Rpk < 0.8㎛를 가지도록 상부층의 표면을 형성하는 것이 바람직하다.With respect to the roughness, it is preferable to form the surface of the upper layer so as to have the roughness parameters Rz < 5 and / or Rpk < 0.8 mu m in order to further improve its properties.

입증된 방식에서, 금속-함유 및/또는 금속을 포함하지 않는 DLC층은 PA-CVD법에 의해 제조될 수 있다.In a proven way, a DLC layer that does not contain metal-containing and / or metal can be produced by the PA-CVD method.

또한, 본 발명은 전술한 바와 같은 적어도 하나의 슬라이딩 요소와 상대 작동 요소의 조합에 관계되고, 특히, 내연 기관의 실린더 또는 실린더 라이너와 관련되고, 특히 디젤 엔진 또는 고출력 과급기를 가진 불꽃-점화 기관에 관련되며, 상대 작동 요소는 철기(iron-based)이다. The present invention also relates to a combination of at least one sliding element and a counter-operative element as described above, and more particularly to a cylinder-or cylinder liner of an internal combustion engine, and more particularly to a spark-ignition engine with a diesel engine or a high- And the relative operating element is iron-based.

본 발명에 따르면, 개시된 코팅은 Me(CxNy) 층이 CrN층과 DLC층 사이의 중간 층으로서 제공될 때 특히 양호한 특성을 나태는 것을 보여준다. 이러한 층 구조를 사용한 시험들은 슬라이딩 요소 특히, 피스톤 링의 표면의 마모 특성이 Cr 접착층과 DLC 상부층을 구비하는 알려진 구조와 비교하여 향상되었음을 나타낸다. 이것은 내구 연한을 엄청나게 향상시킬 수 있다. 또한, 시험들은 상대적 기능 계수를 엄청나게 감소시킬 수 있음을 보여준다.According to the present invention, the disclosed coatings show particularly good properties when a Me (C x N y ) layer is provided as an intermediate layer between the CrN layer and the DLC layer. Tests using this layered structure indicate that the wear characteristics of the sliding elements, particularly the surfaces of the piston rings, are improved compared to known structures comprising a Cr adhesive layer and a DLC top layer. This can dramatically improve durability. Tests also show that the relative functional coefficients can be drastically reduced.

도 1은 본 발명의 바람직한 예시적 실시예에 따른 층 구조를 도시한다.
도 2는 피스톤 링과 실린더 라이너에 상대 마모를 나타내는 그래프이다.
도 3은 다른 층 시스템들의 상대 마찰 계수를 나타내는 그래프이다.
Figure 1 shows a layer structure according to a preferred exemplary embodiment of the present invention.
2 is a graph showing the relative wear of the piston ring and the cylinder liner.
3 is a graph showing relative friction coefficients of different layer systems.

도 1에 도시된 바와 같이, CrN층(12)은 슬라이딩 요소의 기본 물질(10)에 부착된다. 도 1에 도시된 접착층(14)은 반드시 제공될 필요는 없다. 특히, 이것은 생략되는 것이 바람직하다. 또한, Me(CxNy) 중간 층(16)에 의해, DLC층(18)은 외측의 금속을 포함하지 않는 DLC층에 마련된다. As shown in FIG. 1, the CrN layer 12 is attached to the base material 10 of the sliding element. The adhesive layer 14 shown in Fig. 1 does not necessarily have to be provided. In particular, this is preferably omitted. In addition, the Me (C x N y ) intermediate layer 16 provides the DLC layer 18 with a DLC layer that does not contain the outside metal.

상기 접착 층(14) 없이 이러한 유형의 구조물을 이용한 실험이 수행되어 비교예와 비교되었다. 아래 표는 층 시스템을 나타낸다.Experiments using this type of structure without the adhesive layer 14 were performed and compared with the comparative example. The table below shows the layer system.

층 구조
Layer structure
총 층 두께Total layer thickness
기재materials 러닝 표면(Running surface)Running surface 접착 층
Adhesive layer
하부구조Infrastructure 중간 층Intermediate layer 탑 층Top floor [㎛][Mu m]
DLC 시리즈DLC series Cr
Cr
DLCDLC 3.53.5
CNDLC01CNDLC01 -
-
CrN - 01CrN-01 Me(CN)xMe (CN) x DLCDLC 8.88.8
CNDLC02CNDLC02 Cr
Cr
CrON - 02CrON-02 CrCr DLCDLC 14.514.5
CNDLC03CNDLC03 Cr
Cr
Cr-N - 03Cr-N-03 CrCr DLCDLC 14.614.6
CNDLC04CNDLC04 Cr
Cr
CrON - 04CrON-04 CrCr DLCDLC 14.314.3

여기서, 시스템 "DLC 시리즈"는 CrN이 없는 표준 DLC층 시스템이다. 이러한 층 시스템들은 피스톤 링에 부가되었고, 윤활 환경에서 연마 주철 실린더 라이너와 조합하여 마찰 운동학적 행동이 조사되었다. 도 2는 피스톤 링(상부에서)과 실린더 라이너를 위한 상대 마모값을 보여준다. 도시된 백분율 값들은 실험이 끝난 후 남아 있는 원래의 DLC 층의 백분율을 의미한다. 이러한 값이 100% 이상이면, DLC층에 더하여, CrN 또는 CrON 층 역시 적어도 부분적으로 마모된다. 가장 높은 마모 값은 실린더 라이너의 상대 마모를 위한 기준값으로서 사용됨으로써 100 퍼센트로서 정의된다.Here, the system "DLC series" is a standard DLC layer system without CrN. These layer systems were added to the piston ring and friction kinetic behavior was investigated in combination with an abrasive cast iron cylinder liner in a lubrication environment. Figure 2 shows the relative wear values for the piston ring (at the top) and the cylinder liners. The percentages shown represent the percentage of the original DLC layer remaining after the experiment. If this value is more than 100%, in addition to the DLC layer, the CrN or CrON layer is also at least partially worn. The highest wear value is defined as 100 percent by being used as a reference value for the relative wear of the cylinder liner.

도 2를 참조하면, Me(CxNy) 중간 층를 가진 본 발명에 따른 코팅은 가장 낮은 상대 마모를 가진다. 실린더 라이어너 대한 마모의 경우, 알려진 DLC 코팅만이 더 낮은 값을 초래한다. 그러나, 실린더 라이너의 마모 역시 본 발명에 따른 예시를 위해 수용할 만한 범위이다. Referring to FIG. 2, the coating according to the present invention with the Me (C x N y ) intermediate layer has the lowest relative wear. In the case of cylinder liner abrasion, only known DLC coatings result in lower values. However, wear of the cylinder liners is also an acceptable range for the purposes of the present invention.

마찰 계수에 대한 검사 역시 수행되었고 그 결과는 도 3에 도시된다. 여기서, 본 발명에 따른 예는 가장 낮은 상대 마찰 계수를 가진다. 따라서, 이러한 요구조건 역시 비교적으로 낮은 마모 요구 조건에 부가하여 긴 수명 연한을 달성한다.
A test for the coefficient of friction was also performed and the results are shown in Fig. Here, the example according to the present invention has the lowest relative friction coefficient. Therefore, this requirement also achieves a long service life in addition to a relatively low wear requirement.

12...CrN 층 14...접착 층
16...중간 층 18...DLC 층
12 ... CrN layer 14 ... adhesive layer
16 ... intermediate layer 18 ... DLC layer

Claims (11)

내측의 CrN층, 중간의 Me(CxNy)층, 및 외측의 DLC층을 각각 가진 코팅을 구비하는 주철 또는 금속으로 제조된 슬라이딩 요소에 있어서,
상기 DLC층은 금속-함유 하부구조층과 금속을 포함하지 않는 DLC 상부층으로 구성되고;
상기 CrN층의 경도는 1100-1900 HV 0.002 및/또는 상기 금속을 포함하지 않는 DLC 상부층의 경도는 1700-2900 HV 0.002 및/또는 상기 금속-함유 하부구조층의 경도는 800-1600 HV 0.002이며;
상기 Me는 텅스텐, 크로뮴, 티탄 또는 규소이고, x 및 y의 양쪽 모두는 0~99 원자%의 범위인 것을 특징으로 하는 슬라이딩 요소.
In a sliding element made of cast iron or metal having a coating with a respective inner CrN layer, a middle Me (C x N y ) layer, and an outer DLC layer,
The DLC layer comprises a metal-containing substructure layer and a DLC upper layer that does not contain a metal;
The hardness of the CrN layer is 1100-1900 HV 0.002 and / or the hardness of the DLC upper layer not containing the metal is 1700-2900 HV 0.002 and / or the hardness of the metal-containing substructure layer is 800-1600 HV 0.002;
Wherein Me is tungsten, chromium, titanium or silicon, and both x and y are in the range of 0 to 99 atomic%.
삭제delete 청구항 1에 있어서,
상기 금속-함유 하부구조층 및/또는 상기 금속을 포함하지 않는 DLC 상부층은 수소를 포함하는 것을 특징으로 하는 슬라이딩 요소.
The method according to claim 1,
Wherein the metal-containing substructure layer and / or the DLC upper layer that does not comprise the metal comprises hydrogen.
청구항 1에 있어서,
상기 금속-함유 하부구조층은 나노크리스탈 금속카바이드 침전물을 구비하는 것을 특징으로 하는 슬라이딩 요소.
The method according to claim 1,
Wherein said metal-containing substructure layer comprises a nanocrystalline metal carbide precipitate.
청구항 1에 있어서,
상기 CrN층의 두께는 1-30㎛ 및/또는 상기 Me(CxNy)층의 최대 두께는 2㎛ 및/또는 전체 층들의 두께는 5-40㎛인 것을 특징으로 하는 슬라이딩 요소.
The method according to claim 1,
The thickness of the CrN layer is 1-30㎛ and / or wherein Me (C x N y) the maximum thickness of the layer is 2㎛ and / or thickness of the entire layer is a sliding element, characterized in that 5-40㎛.
청구항 1에 있어서,
상기 DLC 상부층의 거칠기는 Rz < 5㎛ 및/또는 Rpk < 0.8㎛인 것을 특징으로 하는 슬라이딩 요소.
The method according to claim 1,
Wherein the DLC upper layer has a roughness Rz < 5 [mu] m and / or Rpk < 0.8 [mu] m.
청구항 1에 있어서,
상기 CrN층은 금속 증착법에 의해 및/또는 상기 금속-함유 하부구조층 및/또는 상기 금속을 포함하지 않는 DLC 상부층은 PA-CVD법에 의해 형성된 것을 특징으로 하는 슬라이딩 요소.
The method according to claim 1,
Wherein the CrN layer is formed by a metal deposition process and / or the DLC upper layer not comprising the metal-containing substructure layer and / or the metal is formed by PA-CVD.
청구항 4에 있어서,
상기 나노크리스탈 금속카바이드 침전물은 WC, CrC, SiC, GeC 또는 TiC를 포함하는 것을 특징으로 하는 슬라이딩 요소.
The method of claim 4,
Wherein the nanocrystalline metal carbide precipitate comprises WC, CrC, SiC, GeC, or TiC.
청구항 1 또는 청구항 3 내지 청구항 8 중 어느 한 항에 있어서,
상기 슬라이딩 요소는 피스톤 링인 것을 특징으로 하는 슬라이딩 요소.
The method according to any one of claims 1 or 3 to 8,
Characterized in that the sliding element is a piston ring.
청구항 9의 피스톤 링; 및
상기 피스톤 링과 접촉되도록 구성된 내연 기관의 실린더 또는 실린더 라이너를 포함하는 조립체.
The piston ring of claim 9; And
And a cylinder or cylinder liner of the internal combustion engine configured to contact the piston ring.
청구항 1 또는 청구항 3 내지 청구항 8 중 어느 한 항의 슬라이딩 요소; 및
상기 슬라이딩 요소와 맞물려 접촉되는 철계(iron-based) 작동 요소를 구비하는 조립체.
A sliding element according to any one of claims 1 to 7, And
And an iron-based actuating element in engagement with the sliding element.
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BR112012010336B1 (en) 2019-09-03

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